Blue light faraday rotation device

ABSTRACT

A Faraday rotation device includes a light source configured to transmit a light beam; a first rotation stage polarizer configured to forward the light beam from the light source at a predetermined reference polarization angle; a quartz cell configured to receive the light beam from the first rotation stage polarizer at the predetermined reference polarization angle; one or more stacked ring permanent magnets coaxially fitted around the quartz cell; a stepper motor configured to adjust a rotational motion of a second rotation stage polarizer connected to the stepper motor, wherein the second rotation stage polarizer is configured to change a polarization angle of the light beam received from the quartz cell; a light detector; and an electronic circuit board configured to record a change in angle between the predetermined reference polarization angle and the changed polarization angle.

BACKGROUND Technical Field

The present invention relates to a Faraday rotator device and a methodof recording a Faraday rotation angle.

Description of the Related Art

The “background” description provided herein is for the purpose ofgenerally presenting the context of the disclosure. Work of thepresently named inventors, to the extent it is described in thisbackground section, as well as aspects of the description which may nototherwise qualify as prior art at the time of filing, are neitherexpressly or impliedly admitted as prior art against the presentinvention.

It has previously been established that if an isotropic transparentmaterial, such as a solid, liquid, or gas organic or inorganic materialis placed in a strong uniform magnetic field and a beam of linearlypolarized light is passed coaxially and parallel with the direction ofmagnetic field lines through the isotropic transparent material, then asignificant rotation in the direction of polarization of the transmittedlight is observed. See P. N. Schatz and A. J. McCaffery, Q. Rev., Chem.Soc. 23, 552 (1969); A. Corney, Atomic and Laser Spectroscopy˜Clarendon,Oxford, 1988, Chap. 15; D. Budker, V. Yashchuk, and M. Zolotorev,‘Nonlinear magneto-optic effects with ultra-narrow widths,” Phys. Rev.Lett. 8˜26, 5788-5791 (1998); C. Y. Chang, L. Wang, J. T. Shy, C. E.Lin, and C. Chou, Rev. Sci. Instrum. 82, 063112 (2011); and J. T. Singh,P. A. M. Dolph, W. A. Tobias, T. D. Averett, A. Kelleher, K. E. Mooney,V. V. Nelyubin, Y. Wang, Y. Zheng, and G. D. Cates, Phys. Rev. C 91,055205 (2015), each incorporated herein by reference in their entirety.This rotation is commonly known as a Faraday rotation, which isdifferent from the optical rotation experienced by linearly polarizedlight passing through chiral transparent samples without the effect of amagnetic field.

The Faraday rotation can be explained by imagining linearly polarizedlight as the coherent superposition of two opposite components of thenet polarization that have different frequencies. If one of thepolarized light components has a frequency ω+ω_(L) possessing arefractive index n₊ then the other component has a frequency

ω−ω_(L) with a refractive index n⁻.

where ω_(L) is the Larmor frequency and is directly related to electronoscillations within the atoms, due to their interaction with an externalmagnetic field B and is given as:

$\begin{matrix}{\omega_{L} = {\frac{e}{m}B}} & (21)\end{matrix}$

Where e: charge of the oscillating electrons

-   -   m: mass of the oscillating electrons    -   B: magnetic flux density

Mathematically, the angle of rotation ϕ (in degrees) can be given interms of the refractive indices of polarized light components (n₊, n⁻),the speed of light c, the magnetic flux density B and the frequency oftransmitted light ω as:

$\begin{matrix}{\Phi = {{\frac{\omega \left( {n_{+} - n_{-}} \right)}{2\; c}B} = {VBL}}} & (2)\end{matrix}$

The right hand side of equation (2) is the common form of the Faradayrotation angle equation where L is the length of the transparentmaterial (cell length), and V is the Verdet's constant (degrees ofrotation/Tesla.m) which is given as:

$\begin{matrix}{V = {{- \frac{e\; \lambda}{2\; {mc}}}\frac{dn}{d\; \lambda}}} & (3)\end{matrix}$

where

$\frac{dn}{d\; \lambda} = {- \frac{2\; B}{\lambda^{3}}}$

is the dispersion of the refractive index of the transparent material,which is derived from the Cauchy equation

$\left( {n = {A + \frac{B}{\lambda^{2}}}} \right).$

Note that B in the dispersion equation above is not the magnetic fieldflux, but rather it is one of Cauchy's constants and is dependent on theintrinsic optical properties of the transparent material. Bysubstituting the dispersion equation in equation (3), a clear inversedependence of Verdet's constant on the square of the wavelength oftransmitted light can be deduced. In other words, the Faraday Rotationangle for a certain isotropic transparent sample is expected to beoptimal for transmitted light of a shorter wavelength for a relativelylong cell, as well as for a high magnetic field flux B. See I. B.Khriplovich and S. K. Lamoreaux, “CP Violation without Strangeness. TheElectric Dipole Moments of Particles, Atoms and Molecules,”Springer-Verlag, New York, 1997, incorporated herein by reference in itsentirety.

SUMMARY

In one embodiment, a Faraday rotation device includes a light sourceconfigured to transmit a light beam; a first rotation stage polarizerconfigured to forward the light beam from the light source at apredetermined reference polarization angle; a quartz cell configured toreceive the light beam from the first rotation stage polarizer at thepredetermined reference polarization angle; one or more stacked ringpermanent magnets coaxially fitted around the quartz cell, the one ormore stacked ring permanent magnets configured to create a magneticfield encircling the quartz cell and rotate the light beam; a steppermotor configured to adjust a rotational motion of a second rotationstage polarizer connected to the stepper motor, wherein the secondrotation stage polarizer is configured to change a polarization angle ofthe light beam received from the quartz cell; a light detectorconfigured to detect the rotated light beam; and an electronic circuitboard configured with circuitry to control the light source, the lightdetector, and the stepper motor, and to record a change in angle betweenthe predetermined reference polarization angle and the changedpolarization angle.

The foregoing paragraphs have been provided by way of generalintroduction, and are not intended to limit the scope of the followingclaims. The described embodiments, together with further advantages,will be best understood by reference to the following detaileddescription taken in conjunction with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete appreciation of the disclosure and many of the attendantadvantages thereof will be readily obtained as the same becomes betterunderstood by reference to the following detailed description whenconsidered in connection with the accompanying drawings, wherein:

FIG. 1 is a schematic diagram of a Faraday rotation device according toone embodiment;

FIG. 2A illustrates a side view of a quartz cell according to oneembodiment;

FIG. 2B illustrates a perspective view of a quartz cell according to oneembodiment;

FIG. 3 illustrates a Faraday rotation device connected to a steppermotor and a circuit board according to one embodiment;

FIG. 4 is a schematic diagram of an exemplary data processing systemaccording to one embodiment;

FIG. 5 illustrates an implementation of a central processing unit (CPU)according to one embodiment; and

FIG. 6 is a flowchart for a method of recording a Faraday rotation angleaccording to one embodiment.

DETAILED DESCRIPTION

The following descriptions are meant to further clarify the presentdisclosure by giving specific examples and embodiments of thedisclosure. These embodiments are meant to be illustrative rather thanexhaustive. The full scope of the disclosure is not limited to anyparticular embodiment disclosed in this specification, but rather isdefined by the claims.

It will be appreciated that in the development of any such actualimplementation, numerous implementation-specific decisions need to bemade in order to achieve the developer's specific goals, such ascompliance with application- and business-related constraints, and thatthese specific goals will vary from one implementation to another andfrom one developer to another.

FIG. 1 is a schematic diagram of a Faraday rotation device 100 accordingto embodiments described herein. A light-emitting diode (LED) 1, such asa GaN-based blue LED is used as the light source. As used herein, asolid state LED light source refers to a type of light source using anelectroluminescence phenomenon in which a material emits light inresponse to passage of an electric current or in response to a strongelectric field. Examples of light sources include, but are not limitedto semiconductor light-emitting diodes (LEDs), organic light-emittingdiodes (OLEDs), polymer light-emitting diodes (PLEDs), and monolithiclight-emitting diodes (MLEDs).

In one example, LED 1 is an epoxy-encased LED of 465 nm, such as anLED465E. In one embodiment, LEDs 1 that encompass the blue regionwavelength range of 400-480 nm can be used.

An iris 2 (also called a pinhole), such as an Iris Diaphragm ID12/M ofadjustable diameter is used to initially collimate the LED 1 outputlight. The output of the iris is further focused using an asphericallens 3, such as an uncoated Aspheric Lens of focal length from 2 to 20mm, 3 to 18 mm, 4 to 15 mm, 5 to 12 mm, 6 to 10 mm, 7 to 9 mm, orpreferably about 8 mm of adjustable focusing to achieve a desiredcollimated light beam.

After focusing, the light is passed through a first rotation stagepolarizer 4, which is kept at a predetermined reference polarizationangle. An exemplary predetermined reference polarization angle is 0-10degrees. However, a specific polarization angle is of littlesignificance since it is simply a starting point to determine a changein rotational motion or angle subsequently calculated.

The linearly polarized light passes through a quartz cell 7 ofapproximately 13 mm in diameter and 10 cm in length. However, otherquartz cell 7 sizes are contemplated by embodiments described herein,such as a diameter of 8-20 mm and a length of 5-20 cm. The quartz cell 7is filled with a gaseous or transparent liquid, such as cesium, iodine,or rubidium and is coaxially inserted within a magnet such as a 2- or3-stacked ring (e.g., multi-stacked ring) permanent magnet 6, such as aNeodymium Ring Magnet RX08X0. This provides a magnetic field strength inthe range of 10,000-15,000 Ga or 11,000-14,000 Ga. In particular, amagnetic field strength of 13,400 Ga inside the quartz cell 7 encirclesand is parallel to the transmitted light.

As the transmitted light exits the quartz cell 7 within the 2- or3-stacked ring permanent magnet 6, a second rotation stage polarizer 5,such as a Polarizer LPVISE100-A is initially at the same referencepolarization angle as the first rotation stage polarizer 4. A photodiode8, such as a silicon photodiode FDS10X10 receives the light signal.

FIG. 2A illustrates a side view of the quartz cell 7 positioned insidethe stacked ring permanent magnet 6. FIG. 2B illustrates a perspectiveview of the quartz cell 7 positioned inside the stacked ring permanentmagnet 6. A first small hole 310 on the circular entrance of the quartzcell 7 and a second small hole 320 on the exit side of the quartz cell 7are used to connect a dry vacuum pump to evacuate air and to flush andchange a sample. An exemplary diameter size for the first small hole 310and the second small hole 320 can be in the range of 0.10-1.0 mm. Asensitive pressure gauge can be connected to either hole to recordentrapped sample pressure.

FIG. 3 illustrates the Faraday rotation device 100 connected to astepper motor 9 and a circuit board 10. As transmitted light exits thequartz cell 7 within the 2- or 3-stacked ring permanent magnet 6, thesecond rotation stage polarizer 5 is made initially at the samereference polarization angle as the first rotation stage polarizer 4.The second rotation stage polarizer 5 is hooked to the stepper motor 9,such as a stepper motor 5V MIKROE-1530. The stepper motor 9automatically changes the polarizer angle, depending on the light signalreceived by the photodiode 8.

Stepper motor 9 preferably operates over two stages. In a first stage,the stepper motor 9 operates in a half-step mode. As a result, the stepangle of the stepper motor 9 yields a sensitivity of 0.09 degrees. In asecond stage, a sensitivity of 0.01 degrees is achieved by connectingthe shaft of the stepper motor 9 to a gearbox to convert the 0.09 degreesensitivity to less than 0.01 degrees. Stepper motor 9 can operate atother exemplary stages, such as a three-stage stepper motor or afour-stage stepper motor.

Circuit board 10, such as a Microchip® PIC18F2550 MIDROE-647 isconnected to the LED 1, the photodiode 8, and the stepper motor 9, andis used to control the Faraday rotation device 100. Parameters of theLED 1 light source, such as the intensity, wavelength, angle etc. arecontrolled by the circuit board 10. Parameters of the photodiode 8, suchas timing with the LED 1 light source and the stepper motor 9 are alsocontrolled by the circuit board 10. Parameters of the stepper motor 9,such as timing and angle of the second polarizer 5 are also controlledby the circuit board 10.

Embodiments herein describe the mechanism for recording the Faradayrotation angle. The focused light is transmitted through the firstrotation stage polarizer 4, which is fixed at a predetermined referenceangle ϕ_(o)=0. The linearly polarized light is aligned to pass throughthe quartz cell 7, which is surrounded by a high magnetic field sourceproduced by the stacked ring permanent magnet 6. As a result, a rotationof the polarization direction of the transmitted light occurs by anangle of ϕ. In an example given for illustrative purposes only, arotation of the polarization direction of the transmitted light canrange from 0.1-10 degrees.

The stepper motor 9 is connected to the second rotation stage polarizer5. The second rotation stage polarizer 5 is initially at the samereference polarization angle as the first rotation stage polarizer 4.The stepper motor 9 automatically changes the polarization angle andhence changes the polarization angle of the second rotation stagepolarizer 5, depending upon a light signal received by the photodiode 8.A feedback loop from the photodiode instructs the polarizer to rotate toa maximal/minimal photodiode signal.

The stepper motor 9 in sync with the received detector signal undergoesa rotational motion of the second rotation stage polarizer 5, whichsearches for a minimal signal. A minimal signal is the lowest lightintensity detected by the photodiode 8. It becomes a minimal signalduring the rotation of the second rotation stage polarizer 5 relative tothe first rotation stage polarizer 4. When the minimal signal islocated, the stepper motor 9 stops rotating and the actual angle movedfrom the reference point of the first rotation stage polarizer 4 isdigitally recorded as the Faraday rotation angle of that specific sampleat the utilized LED wavelength.

Circuit board 10 is configured with circuitry to control the lightsource (LED 1), the light detector (photodiode 8), and the stepper motor9, and to record a change in angle between the predetermined referencepolarization angle and the changed polarization angle. The circuit board10 triggers the stepper motor 9 and the photodiode 8 with the samecommand function. The photodiode 8 takes a reading while the steppermotor 9 rotates for a full revolution to determine the minimum andmaximum detected light intensities. The LED 1 can be replaced with asimilar LED 1 of a different wavelength covering the range of 400-480nm. Therefore, it is possible to record the Faraday rotation atdifferent wavelengths within the blue region. In addition, theportability of the setup is evident as the power supplier for all setupcomponents can be sustained using a simple DC battery.

FIG. 4 is a schematic diagram of an exemplary data processing system,such as microchip 10 according to aspects of the disclosure describedherein for operating the Faraday rotator device. The data processingsystem is an example of a computer in which code or instructionsimplementing the processes of the illustrative embodiments can belocated.

In FIG. 4, data processing system 400 employs an applicationarchitecture including a north bridge and memory controller hub (NB/MCH)425 and a south bridge and input/output (I/O) controller hub (SB/ICH)420. The central processing unit (CPU) 430 is connected to NB/MCH 425.The NB/MCH 425 also connects to the memory 445 via a memory bus, andconnects to the graphics processor 450 via an accelerated graphics port(AGP). The NB/MCH 425 also connects to the SB/ICH 420 via an internalbus (e.g., a unified media interface or a direct media interface). TheCPU 430 can contain one or more processors and even can be implementedusing one or more heterogeneous processor systems.

FIG. 5 illustrates an implementation of CPU 430. In one implementation,an instruction register 538 retrieves instructions from a fast memory539. At least part of these instructions are fetched from an instructionregister 538 by a control logic 536 and interpreted according to theinstruction set architecture of the CPU 430. Part of the instructionscan also be directed to a register 532. In one implementation theinstructions are decoded according to a hardwired method, and in anotherimplementation the instructions are decoded according to a microprogramthat translates instructions into sets of CPU configuration signals thatare applied sequentially over multiple clock pulses. After fetching anddecoding the instructions, the instructions are executed using anarithmetic logic unit (ALU) 534 that loads values from the register 532and performs logical and mathematical operations on the loaded valuesaccording to the instructions. The results from these operations can befed back into the register 532 and/or stored in a fast memory 539.According to aspects of the disclosure, the instruction set architectureof the CPU 430 can use a reduced instruction set computer (RISC), acomplex instruction set computer (CISC), a vector processorarchitecture, or a very long instruction word (VLIW) architecture.Furthermore, the CPU 430 can be based on the Von Neuman model or theHarvard model. The CPU 430 can be a digital signal processor, an FPGA,an ASIC, a PLA, a PLD, or a CPLD. Further, the CPU 430 can be an x86processor by Intel or by AMD; an ARM processor; a Power architectureprocessor by, e.g., IBM; a SPARC architecture processor by SunMicrosystems or by Oracle; or other known CPU architectures.

Referring again to FIG. 4, the data processing system 400 can includethe SB/ICH 420 being coupled through a system bus to an I/O Bus, a readonly memory (ROM) 456, universal serial bus (USB) port 464, a flashbinary input/output system (BIOS) 468, and a graphics controller 458.PCI/PCIe devices can also be coupled to SB/ICH 420 through a PCI bus462.

The PCI devices can include, for example, Ethernet adapters, add-incards, and PC cards for notebook computers. The Hard disk drive 460 andCD-ROM 466 can use, for example, an integrated drive electronics (IDE)or serial advanced technology attachment (SATA) interface. In oneimplementation the I/O bus can include a super I/O (SIO) device.

Further, the hard disk drive (HDD) 460 and optical drive 466 can also becoupled to the SB/ICH 420 through a system bus. In one implementation, akeyboard 470, a mouse 472, a parallel port 478, and a serial port 476can be connected to the system bus through the I/O bus. Otherperipherals and devices can be connected to the SB/ICH 420 using a massstorage controller such as SATA or PATA, an Ethernet port, an ISA bus, aLPC bridge, SMBus, a DMA controller, and an Audio Codec.

Moreover, the present disclosure is not limited to the specific circuitelements described herein, nor is the present disclosure limited to thespecific sizing and classification of these elements. For example, theskilled artisan will appreciate that the circuitry described herein maybe adapted based on changes on battery sizing and chemistry, or based onthe requirements of the intended back-up load to be powered. Embodimentsdescribed herein can be a combination of hardware and software, andprocessing circuitry by which the software is implemented.

The functions and features described herein can also be executed byvarious distributed components of a system. For example, one or moreprocessors can execute these system functions, wherein the processorsare distributed across multiple components communicating in a network.The distributed components can include one or more client and servermachines, which can share processing, such as a cloud computing system,in addition to various human interface and communication devices (e.g.,display monitors, smart phones, tablets, personal digital assistants(PDAs)). The network can be a private network, such as a LAN or WAN, orcan be a public network, such as the Internet. Input to the system canbe received via direct user input and received remotely either inreal-time or as a batch process. Additionally, some implementations canbe performed on modules or hardware not identical to those described.Accordingly, other implementations are within the scope that can beclaimed.

Distributed performance of the processing functions can also be realizedusing grid computing or cloud computing. Many modalities of remote anddistributed computing can be referred to under the umbrella of cloudcomputing, including: software as a service, platform as a service, dataas a service, and infrastructure as a service. Cloud computing generallyrefers to processing performed at centralized locations and accessibleto multiple users who interact with the centralized processing locationsthrough individual terminals.

FIG. 6 illustrates an exemplary flowchart for a method 600 of recordinga Faraday rotation angle according to an aspect of the presentdisclosure. Method 600 includes programmable computer-executableinstructions, that when used in combination with the above-describedhardware devices, carry out the steps of method 600.

FIG. 6 is a flowchart for the method 600 of recording a Faraday rotationangle according to an aspect of the present disclosure. In step S610, alight beam is transmitted from a light source through a first rotationstage polarizer. A first polarization light beam is obtained at apredetermined reference angle.

In step S620, the first polarization light beam is transmitted through aquartz cell. The quartz cell is surrounded by one or more stacked ringpermanent magnets.

In step S630, a polarization direction of the transmitted firstpolarization light beam is rotated by a predetermined rotation angle. Instep S640, a second rotation stage polarizer is rotated, via a stepper.In step S650, the first polarization light beam is received at thesecond rotation stage polarizer.

In step S660, a minimal signal is searched from a second polarizationlight beam emitted from the second rotation stage polarizer, via aphotodetector. In step S670, a rotation of the stepper is halted whenthe minimal signal is detected. In step S680, the rotation angle betweenthe predetermined reference angle and an angle at which the rotation ofthe stepper halted is recorded.

Several advantages are realized using the embodiments described hereinfor a Faraday rotator device. The faraday rotator device describedherein using an LED light source, such as a blue LED light sourceinstead of a laser light source or a lamp light source. A permanentmagnet, such as a neodymium ring permanent magnet is preferably usedinstead of an electromagnet or a solenoid. The Faraday rotator devicedescribed herein can be used to measure Faraday rotation in gases sinceit depends upon transmitted light instead of reflected light.

The combination of a photodiode, such as photodiode 8 and a steppermotor, such as stepper motor 9 is more sensitive due to the coupling ofthe photodiode 8 and the stepper motor 9. The Faraday rotator devicedescribed herein is more economical, is less complicated, and isportable. There is no need for signal modulation using embodimentsdescribed herein.

Embodiments described herein include the following aspects.

(1) A Faraday rotation device includes a light source configured totransmit a light beam; a first rotation stage polarizer configured toforward the light beam from the light source at a predeterminedreference polarization angle; a quartz cell configured to receive thelight beam from the first rotation stage polarizer at the predeterminedreference polarization angle; one or more stacked ring permanent magnetscoaxially fitted around the quartz cell, the one or more stacked ringpermanent magnets configured to create a magnetic field encircling thequartz cell and rotate the light beam; a stepper motor configured toadjust a rotational motion of a second rotation stage polarizerconnected to the stepper motor, wherein the second rotation stagepolarizer is configured to change a polarization angle of the light beamreceived from the quartz cell; a light detector configured to detect therotated light beam; and an electronic circuit board configured withcircuitry to control the light source, the light detector, and thestepper motor, and to record a change in angle between the predeterminedreference polarization angle and the changed polarization angle.

(2) The Faraday rotation device of (1), further includes an irisdiaphragm configured to collimate the light beam outputted from thelight source.

(3) The Faraday rotation device of either one of (1) or (2), furtherincludes an aspheric lens configured to focus the light beam outputtedfrom the light source.

(4) The Faraday rotation device of any one of (1) through (3), whereinthe light source comprises a light-emitting diode (LED).

(5) The Faraday rotation device of any one of (1) through (4), whereinthe LED is configured to operate within a wavelength range of 400-480nm.

(6) The Faraday rotation device of any one of (1) through (5), whereinthe light detector comprises a silicon photodiode.

(7) The Faraday rotation device of any one of (1) through (6), whereinthe one or more stacked ring permanent magnets are configured to producea magnetic field inside the quartz cell parallel to the transmittedlight beam from the light source.

(8) The Faraday rotation device of any one of (1) through (7), whereinthe stepper motor is a two-stage stepper motor.

(9) A method of recording a Faraday rotation angle includes transmittinga light beam from a light source through a first rotation stagepolarizer at a predetermined reference angle to obtain a firstpolarization light beam; transmitting the first polarization light beamthrough a quartz cell surrounded by one or more stacked ring permanentmagnets; rotating, via the one or more stacked ring permanent magnets, apolarization direction of the transmitted first polarization light beamby a predetermined rotation angle; rotating a second rotation stagepolarizer, via a stepper; receiving the first polarization light beam atthe second rotation stage polarizer; searching, via a photodetector, fora minimal signal from a second polarization light beam emitted from thesecond rotation stage polarizer; halting a rotation of the stepper whenthe minimal signal is detected; and recording, via an electronic circuitboard, a rotation angle between the predetermined reference angle and anangle at which the rotation of the stepper halted.

(10) The method of recording a Faraday rotation angle of (9), furtherincludes collimating, via an iris diaphragm, the light beam outputtedfrom the light source.

(11) The method of recording a Faraday rotation angle of either one of(9) or (10), further includes focusing, via an aspheric lens, the lightbeam outputted from the light source.

(12) The method of recording a Faraday rotation angle of any one of (9)through (11), further includes producing, via the one or more stackedring permanent magnets, a magnetic field inside the quartz cell parallelto the transmitted light beam from the light source.

(13) A Faraday rotation device includes a light source configured totransmit a light beam; a first rotation stage polarizer configured toforward the light beam from the light source at a predeterminedreference polarization angle; a quartz cell configured to receive thelight beam from the first rotation stage polarizer at the predeterminedreference polarization angle; one or more stacked ring permanent magnetscoaxially fitted around the quartz cell, the one or more stacked ringpermanent magnets configured to create a magnetic field encircling thequartz cell and rotate the light beam; a stepper motor connected to asecond rotation stage polarizer, wherein the second rotation stagepolarizer is configured to change a polarization angle of the light beamreceived from the quartz cell; a light detector configured to detect therotated light beam; and processing circuitry. The processing circuitryis configured to transmit the light beam from the light source throughthe first rotation stage polarizer to obtain a first polarization lightbeam; transmit the first polarization light beam through the quartzcell; rotate the second rotation stage polarizer, via the stepper;search for a minimal signal from a second polarization light beamemitted from the second rotation stage polarizer; halt a rotation of thestepper when the minimal signal is detected; and record a rotation anglebetween the predetermined reference angle and an angle at which therotation of the stepper halted.

(14) The Faraday rotation device of (13), wherein the light sourcecomprises a light-emitting diode (LED).

(15) The Faraday rotation device of either one of (13) or (14), whereinthe LED is configured to operate within a wavelength range of 400-480nm.

(16) The Faraday rotation device of any one of (13) through (15),wherein the light detector comprises a silicon photodiode.

(17) The Faraday rotation device of any one of (13) through (16),wherein the stepper motor is a two-stage stepper motor.

A number of implementations have been described. Nevertheless, it willbe understood that various modifications may be made without departingfrom the spirit and scope of this disclosure. For example, preferableresults may be achieved if the steps of the disclosed techniques wereperformed in a different sequence, if components in the disclosedsystems were combined in a different manner, or if the components werereplaced or supplemented by other components. The functions, processes,and algorithms described herein may be performed in hardware or softwareexecuted by hardware, including computer processors and/or programmablecircuits configured to execute program code and/or computer instructionsto execute the functions, processes, and algorithms described herein.Additionally, an implementation may be performed on modules or hardwarenot identical to those described. Accordingly, other implementations arewithin the scope that may be claimed.

The foregoing discussion describes merely exemplary embodiments of thepresent disclosure. As will be understood by those skilled in the art,the present disclosure may be embodied in other specific forms withoutdeparting from the spirit or essential characteristics thereof.Accordingly, the disclosure is intended to be illustrative, but notlimiting of the scope of the disclosure, as well as the claims. Thedisclosure, including any readily discernible variants of the teachingsherein, defines in part, the scope of the foregoing claim terminologysuch that no inventive subject matter is dedicated to the public.

1. A blue light Faraday rotation device, comprising: a GaN-based bluelight source configured to transmit a light beam; a first rotation stagepolarizer configured to forward the light beam from the light source ata predetermined reference polarization angle; a cylindrical quartz cellconfigured to receive the light beam from the first rotation stagepolarizer at the predetermined reference polarization angle, thecylindrical quartz cell including a first hole on a circular entrance ofthe cylindrical quartz cell and a second hole on a circular exit of thecylindrical quartz cell, the first hole and the second hole creating atunnel within the cylindrical quartz cell structure and beingconnectable to a dry vacuum pump to evacuate air, and to flush andchange a sample; one or more stacked ring permanent magnets coaxiallyand circumferentially fitted around the cylindrical quartz cell, the oneor more stacked ring permanent magnets configured to create a magneticfield encircling the cylindrical quartz cell and rotate the light beam;a stepper motor configured to adjust a rotational motion of a secondrotation stage polarizer connected to the stepper motor, wherein thesecond rotation stage polarizer is configured to change a polarizationangle of the light beam received from the cylindrical quartz cell; alight detector configured to detect the rotated light beam; and anelectronic circuit board configured with circuitry to control the lightsource, the light detector, and the stepper motor, and to record achange in angle between the predetermined reference polarization angleand the changed polarization angle.
 2. The Faraday rotation device ofclaim 1, further comprising: an iris diaphragm configured to collimatethe light beam outputted from the light source.
 3. The Faraday rotationdevice of claim 1, further comprising: an aspheric lens configured tofocus the light beam outputted from the light source. 4-5. (canceled) 6.The Faraday rotation device of claim 1, wherein the light detectorcomprises a silicon photodiode.
 7. (canceled)
 8. The Faraday rotationdevice of claim 1, wherein the stepper motor is a two-stage steppermotor. 9-17. (canceled)